FR3002334B1 - METHOD AND DEVICE FOR ESTIMATING A NON-DESIRED TANK MOMENT OF AN AIRCRAFT, AND APPLICATIONS TO AIRCRAFT TANGING CONTROL - Google Patents

METHOD AND DEVICE FOR ESTIMATING A NON-DESIRED TANK MOMENT OF AN AIRCRAFT, AND APPLICATIONS TO AIRCRAFT TANGING CONTROL

Info

Publication number
FR3002334B1
FR3002334B1 FR1351382A FR1351382A FR3002334B1 FR 3002334 B1 FR3002334 B1 FR 3002334B1 FR 1351382 A FR1351382 A FR 1351382A FR 1351382 A FR1351382 A FR 1351382A FR 3002334 B1 FR3002334 B1 FR 3002334B1
Authority
FR
France
Prior art keywords
aircraft
tanging
estimating
applications
control
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
FR1351382A
Other languages
French (fr)
Other versions
FR3002334A1 (en
Inventor
Simon Oudin
Guilhem Puyou
Stephane Delannoy
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Operations SAS
Original Assignee
Airbus Operations SAS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Airbus Operations SAS filed Critical Airbus Operations SAS
Priority to FR1351382A priority Critical patent/FR3002334B1/en
Priority to US14/182,743 priority patent/US9120556B2/en
Publication of FR3002334A1 publication Critical patent/FR3002334A1/en
Application granted granted Critical
Publication of FR3002334B1 publication Critical patent/FR3002334B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C19/00—Aircraft control not otherwise provided for
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • G05D1/0816—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability
    • G05D1/0825—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability using mathematical models

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Pure & Applied Mathematics (AREA)
  • Mathematical Physics (AREA)
  • Mathematical Optimization (AREA)
  • Mathematical Analysis (AREA)
  • Algebra (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Automation & Control Theory (AREA)
  • Traffic Control Systems (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Feedback Control In General (AREA)
FR1351382A 2013-02-19 2013-02-19 METHOD AND DEVICE FOR ESTIMATING A NON-DESIRED TANK MOMENT OF AN AIRCRAFT, AND APPLICATIONS TO AIRCRAFT TANGING CONTROL Active FR3002334B1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1351382A FR3002334B1 (en) 2013-02-19 2013-02-19 METHOD AND DEVICE FOR ESTIMATING A NON-DESIRED TANK MOMENT OF AN AIRCRAFT, AND APPLICATIONS TO AIRCRAFT TANGING CONTROL
US14/182,743 US9120556B2 (en) 2013-02-19 2014-02-18 Method and device for estimating an unwanted pitch moment of an aircraft, and applications to the pitch control of the aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1351382A FR3002334B1 (en) 2013-02-19 2013-02-19 METHOD AND DEVICE FOR ESTIMATING A NON-DESIRED TANK MOMENT OF AN AIRCRAFT, AND APPLICATIONS TO AIRCRAFT TANGING CONTROL

Publications (2)

Publication Number Publication Date
FR3002334A1 FR3002334A1 (en) 2014-08-22
FR3002334B1 true FR3002334B1 (en) 2016-07-15

Family

ID=48652240

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1351382A Active FR3002334B1 (en) 2013-02-19 2013-02-19 METHOD AND DEVICE FOR ESTIMATING A NON-DESIRED TANK MOMENT OF AN AIRCRAFT, AND APPLICATIONS TO AIRCRAFT TANGING CONTROL

Country Status (2)

Country Link
US (1) US9120556B2 (en)
FR (1) FR3002334B1 (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
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US9878776B2 (en) * 2014-05-15 2018-01-30 The Boeing Company System and method for optimizing horizontal tail loads
US9821903B2 (en) * 2014-07-14 2017-11-21 The Boeing Company Closed loop control of aircraft control surfaces
EP3224135B1 (en) * 2014-11-25 2020-04-01 Sikorsky Aircraft Corporation Flight control system for a rotary wing aircraft
FR3057370B1 (en) * 2016-10-11 2019-08-23 Airbus Operations METHOD AND SYSTEM FOR CONTROLLING FLIGHT OF AN AIRCRAFT
CN112947539B (en) * 2020-12-17 2023-07-07 中国航空工业集团公司沈阳飞机设计研究所 Method for compensating control surface nonlinearity caused by linear driver

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US3963197A (en) * 1971-12-16 1976-06-15 Messerschmitt-Bolkow-Blohm Gmbh Control device for avoiding the pitching up of missiles or aircraft
US4003533A (en) * 1973-10-01 1977-01-18 General Dynamics Corporation Combination airbrake and pitch control device
US4569494A (en) * 1982-12-23 1986-02-11 The Boeing Company Pitch control of swept wing aircraft
FR2661149B1 (en) * 1990-04-24 1992-08-14 Aerospatiale SYSTEM FOR THE PILOTAGE OF AN AIRPLANE IN TANGAGE.
US5722620A (en) * 1995-05-15 1998-03-03 The Boeing Company Aircraft pitch-axis stability and command augmentation
GB0127254D0 (en) * 2001-11-13 2002-01-02 Lucas Industries Ltd Aircraft flight surface control system
US6648269B2 (en) * 2001-12-10 2003-11-18 Sikorsky Aircraft Corporation Trim augmentation system for a rotary wing aircraft
US6885917B2 (en) * 2002-11-07 2005-04-26 The Boeing Company Enhanced flight control systems and methods for a jet powered tri-mode aircraft
US7284984B1 (en) * 2003-04-09 2007-10-23 Microsoft Corporation Automatic longitudinal pitch trim in aircraft combat simulation
US7108232B2 (en) * 2004-02-05 2006-09-19 Hoh Roger H Helicopter force-feel and stability augmentation system with parallel servo-actuator
US20050242234A1 (en) * 2004-04-29 2005-11-03 The Boeing Company Lifters, methods of flight control and maneuver load alleviation
FR2870942B1 (en) * 2004-05-25 2006-08-25 Airbus France Sas ANTICIPATED MEASUREMENT SYSTEM FOR TURBULENCE UPSTREAM OF AN AIRCRAFT
FR2881849B1 (en) * 2005-02-04 2007-04-06 Airbus France Sas METHOD AND DEVICE FOR CONTROLLING A PLANE IN BLANK
FR2891802B1 (en) * 2005-10-11 2009-03-13 Airbus France Sas METHOD AND DEVICE FOR ATTENUATING THE EFFECTS OF VERTICAL TURBULENCE ON AN AIRCRAFT
US7264199B2 (en) * 2005-10-18 2007-09-04 The Boeing Company Unloaded lift offset rotor system for a helicopter
EP1945501A4 (en) * 2005-11-09 2013-04-24 Morgan Aircraft Llc Aircraft attitude control configuration
US20080237402A1 (en) * 2005-12-19 2008-10-02 Marc Ausman Aircraft trim safety system and backup controls
US8014906B2 (en) * 2006-12-19 2011-09-06 The Boeing Company Multi-axis trim processing
FR2912991B1 (en) * 2007-02-28 2009-12-04 Airbus France METHOD AND DEVICE FOR DYNAMICALLY REDUCING CHARGES GENERATED ON AN AIRCRAFT.
DE102007012425A1 (en) * 2007-03-15 2008-09-18 Airbus Deutschland Gmbh Method and device for finned trimming in an aircraft
FR2916868B1 (en) * 2007-06-01 2009-07-24 Airbus France Sas METHOD AND DEVICE FOR DETERMINING THE DYNAMIC STABILITY MARGIN OF AN AIRCRAFT
US8090485B2 (en) * 2007-11-27 2012-01-03 Embraer S.A. Low-frequency flight control system oscillatory faults prevention via horizontal and vertical tail load monitors
FR2927428B1 (en) * 2008-02-11 2010-02-19 Airbus France METHOD AND DEVICE FOR MITIGATING THE EFFECTS OF VERTICAL TURBULENCE ON AN AIRCRAFT
EP2261116B1 (en) * 2009-06-09 2019-05-22 Sikorsky Aircraft Corporation Automatic trim system for fly-by-wire aircraft with unique trim controllers
DE102009050748A1 (en) * 2009-10-27 2011-05-05 Airbus Operations Gmbh Aircraft with tail fins attached to a central fuselage body and method and control unit for compensating a negative pitching moment
US8718839B2 (en) * 2009-12-06 2014-05-06 Evolved Aircraft Systems, L.L.C. Method and apparatus for automatically controlling aircraft flight control trim systems

Also Published As

Publication number Publication date
FR3002334A1 (en) 2014-08-22
US9120556B2 (en) 2015-09-01
US20140236399A1 (en) 2014-08-21

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